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anti-icing off, is provided by Figure 06−06−5.
NOTE
If ice accumulation is suspected on unprotected surfaces, then reduce the
landing climb gradient values derived from Figure 06−06−5 by 3.1%.
Example:
Associated Conditions:
Airport pressure altitude = 8,000 feet
Temperature = 27°C
Wing & Cowl Anti-Icing = Off
10th Stage Bleeds = Closed
Airplane weight = 15,000 kg (33,069 lb)
The example in Figure 06−06−5 shows that for the above associated conditions, the landing
climb gradient for a landing with flaps 45° is 13.4%.
PERFORMANCE
Approach and Landing Climb
06−06−14
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. LANDING CLIMB GRADIENT (CONT'D)
DFM0606_007 ldg_acu_and_off_405_ha.un
PERFORMANCE
Approach and Landing Climb
06−06−15
REV 66, Feb 01/07
Landing Climb Gradient, Flaps 45° − Anti-Icing Off
Figure 06−06−5
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. LANDING CLIMB GRADIENT (CONT'D)
B. Landing Climb Gradient, Flaps 45° – Anti-Icing On
The landing climb gradient for varying conditions, for a landing with flaps 45° with the
anti-icing on, is provided by Figure 06−06−6.
NOTE
If ice accumulation is suspected on unprotected surfaces, then reduce the
landing climb gradient values derived from Figure 06−06−6 by 3.1%.
Example:
Associated Conditions:
Airport pressure altitude = 10,000 feet
Temperature = –8°C
Cowl Anti-Icing = On
10th Stage Bleeds = Closed
Airplane weight = 15,000 kg (33,069 lb)
The example in Figure 06−06−6 shows that for the above associated conditions, the landing
climb gradient for a landing with flaps 45° is 14.0%.
PERFORMANCE
Approach and Landing Climb
06−06−16
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. LANDING CLIMB GRADIENT (CONT'D)
DFM0606_008 ldg_anti_ice_405_ha.uni
PERFORMANCE
Approach and Landing Climb
06−06−17
REV 66, Feb 01/07
Landing Climb Gradient, Flaps 45° − Anti-Icing On
Figure 06−06−6
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
PERFORMANCE
Approach and Landing Climb
06−06−18
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. INTRODUCTION
The Landing Performance section contains the charts used to obtain the landing performance
data for varying conditions of temperature, airport pressure altitude, and airplane weight for the
specified approach and landing configurations.
2. MAXIMUM ALLOWABLE LANDING WEIGHT
The maximum allowable landing weight is limited by the most restrictive of the following:
• Maximum approved landing weight
(Refer to Chapter 2; LIMITATIONS – STRUCTURAL WEIGHT)
• Runway length available
• Climb requirements
PERFORMANCE
Landing Performance
06−07−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
2. MAXIMUM ALLOWABLE LANDING WEIGHT (CONT'D)
A. Maximum Landing Weight Limited By Climb Requirements –
Approach Flaps 20°/Landing Flaps 45°
The maximum landing weight limited by climb requirements for varying conditions of airport
pressure altitude and temperature for the flaps 20° approach climb configuration and a
subsequent landing flaps 45° configuration, are given in Figure 06−07−1. The chart
incorporates all applicable anti-icing and 10th stage bleeds combinations.
NOTE
If ice accumulation is suspected on unprotected surfaces, then reduce the
maximum landing weight values derived from Figure 06−07−1 by 800 kg
(1,764 lb).
Example: ANTI-ICE ON
Associated Conditions:
Temperature = –8°C
Airport pressure altitude = 4,000 ft
Cowl anti-ice = On
10th stage bleeds = Closed
As shown in the example (Figure 06−07−1, Anti-ice On), the maximum landing weight
limited by climb requirements is 24,900 kg (54,895 lb). The landing weight in this case is
greater than the maximum approved landing weight (Refer to Chapter 2; LIMITATIONS –
STRUCTURAL WEIGHT) and is not considered limiting.
Example: ANTI-ICE OFF
Associated Conditions:
Temperature = 27°C
Airport pressure altitude = 4,000 ft
　
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